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You searched for: (collection:ufnaca OR mediatype:ufnaca) AND -mediatype:collection AND firstTitle:N
[texts]NACA impact basin and water landing tests of a float model at various velocities and weights - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804832&ix=nu&I=0&V=D&pm=1
Keywords: Seaplanes; Aerodynamics--Research
Downloads: 134
[texts]NACA mach number warning device for use in flight - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804356&ix=nu&I=0&V=D&pm=1
Keywords: Mach number; Aerodynamics
Downloads: 145
[texts]New simple interferometer for obtaining quantitatively evaluable flow patterns - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780275&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Interferometers
Downloads: 87
[texts]Nonlinear theory of a hot-wire anemometer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778597&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings; Hot-wire anemometer
Downloads: 127
[texts]Nonstationary gas flow in thin pipes of variable cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804176&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Difference equations; Gas flow
Downloads: 163
[texts]Note on compressibility effects on downwash at the tail at subcritical speeds - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003617581&ix=nu&I=0&V=D&pm=1
Keywords: Compressibility; Aerodynamics--Research
Downloads: 133
[texts]Numerical evaluation by harmonic analysis of the epsilon-function of the Theodorsen arbitrary-airfoil potential theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003595904&ix=nu&I=0&V=D&pm=1
Keywords: Conformal mapping; Harmonic analysis; Aeronautics--Research
Downloads: 111
[texts]Numerical evaluation of the [epsilon]-integral occurring in the Theodorsen arbitrary-airfoil potential theory - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003605363&ix=nu&I=0&V=D&pm=1
Keywords: Conformal mapping; Harmonic analysis; Aeronautics--Research
Downloads: 95
[texts]Numerical evaluation of the wake-survey equations for subsonic flow including the effect of energy addition - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003624211&ix=nu&I=0&V=D&pm=1
Keywords: Wakes (Aerodynamics; Aeronautics--Research
Downloads: 402
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